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Finite-time stabilization of satellite quaternion attitude | ||
| Computational Methods for Differential Equations | ||
| مقاله 4، دوره 3، شماره 4، دی 2015، صفحه 274-283 اصل مقاله (172.38 K) | ||
| نوع مقاله: Research Paper | ||
| نویسندگان | ||
| Mohammad Reza Niknam* ؛ Aghileh Heydari | ||
| Department of Mathematics, Payame Noor University, P.O.Box 19395-3697, Tehran, Iran | ||
| چکیده | ||
| In this paper, a finite-time control scheme is presented for stabilization of the satellite chaotic attitude around its equilibrium point when its attitude is confused by a disturbed torque. Controllers and settling time of stabilizaton are obtained, based on the Lyapunov stability theorem and finite-time control scheme. This method is satisfied for any initial condition. Numerical simulations are presented to illustrate the ability and effectiveness of proposed method. | ||
| کلیدواژهها | ||
| Finite-time stabilization؛ quaternion؛ satellite attitude | ||
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